Effect of thickness, camber, and thickness distribution on airfoil characteristics at Mach numbers up to 1.0
02.10.1952
Sonstige
Keine Angabe
Englisch
Engineering Index Backfile | 1956
|Effect of Airfoil Thickness, Camber and Reynolds Number on Plunging Airfoil Propulsion
British Library Conference Proceedings | 2009
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